IRIDIUM 106, 41917
Orbit data source: Space-Track
IRIDIUM 106, 41917 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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41917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 IRIDIUM 106
1 41917U 17003A 25260.09127645 .00000083 00000-0 22467-4 0 9998
2 41917 86.4021 202.6055 0002678 81.4226 278.7274 14.34218361454060Epoch: 2025-09-17T02:11Z
TLE epoch observation values (Epoch: 2025-09-17T02:11:26.285Z)
Latitude
0.00007°
Longitude
173.47378°
Altitude
780.426 km
Speed
7.464 km/s
True Right ascension
13h 30m 25s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:50:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.545 km
Perigee altitude
772.714 km
Semi-major axis
7,152.767 km
Eccentricity
0.00027
Inclination
86.4021°
RAAN
202.6055°
Arg. of periapsis
81.4226°
True anomaly
278.69707°
Mean anomaly
278.7274°
Eccentric anomaly
278.71223°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000022467
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 106 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-17 20:42:53.327Z | 176.424° S | 2025-09-17 20:47:53.327Z | 58.641° ENE | 44.377° | 2025-09-17 20:51:53.327Z | 5.562° NNE |
| 5 mins | 2025-09-18 07:15:53.327Z | 47.51° ENE | 2025-09-18 07:17:53.327Z | 76.595° E | 19.057° | 2025-09-18 07:20:53.327Z | 116.977° SE |
| 7 mins | 2025-09-18 08:55:53.327Z | 332.995° NNW | 2025-09-18 08:58:53.327Z | 271.463° WNW | 34.61° | 2025-09-18 09:02:53.327Z | 206.649° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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